We present algorithms for attitude guidance and economical digital control of an information satellite at initial modes – during from its separation from a launcher rocket up to its regular attitude stabilization in orbital reference frame. We represent the computer simulation results on the initial orientation modes of a land-survey satellite on sun-synchronous orbit.


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    Title :

    Spacecraft attitude guidance and economical digital control in initial modes


    Contributors:

    Conference:

    ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia


    Published in:

    Publication date :

    2018-12-04


    Size :

    7 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English





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